Attitude control of reentry vehicles in roll channel using single-gimbal control moment gyros and a reaction control system

被引:5
|
作者
Yu, Xiang [1 ]
Liu, Kun [1 ]
机构
[1] Natl Univ Def Technol, Coll Aerosp Sci & Engn, Changsha 410073, Hunan, Peoples R China
基金
中国国家自然科学基金;
关键词
Reentry vehicle; attitude control; single-gimbal control moment gyro; reaction control system; sliding-mode control; fuzzy allocation; hardware-in-the-loop simulation; MOVING-MASS; AERODYNAMIC SURFACES; GUIDANCE LAW; DESIGN; LOGIC;
D O I
10.1177/1687814017737450
中图分类号
O414.1 [热力学];
学科分类号
摘要
A novel roll-channel attitude control scheme using a combination of single-gimbal control moment gyros and a reaction control system is proposed, providing sufficient control torque during the whole reentry process. A scissored-pair configuration is applied to the single-gimbal control moment gyros, which guarantees control torque exclusively along the roll axis and avoids internal singularity. A sliding-mode attitude controller is proposed to meet the requirements of roll-channel attitude stability and disturbance rejection. To obtain an optimal allocation of the commanded torque to the single-gimbal control moment gyros and the reaction control system, an allocation method based on fuzzy reasoning is proposed. To render the design and validation of the control scheme close to reality, the responsiveness of the single-gimbal control moment gyro is considered, and the discrete and delay properties of the reaction control system are included. The steering logic of the single-gimbal control moment gyro and the modulator of the reaction control system are designed, respectively. Numerical simulation is performed to verify the proposed control scheme. Moreover, a hardware-in-the-loop simulation system based on an air-bearing test bed is developed to conduct experiments for convincingly validating the proposed attitude control method. The feasibility and good performance of the proposed control scheme are verified by the results of the numerical simulation and the experiment.
引用
收藏
页数:18
相关论文
共 50 条
  • [31] Attitude adaptive control of satellites using double-gimbal magnetically suspended control moment gyros
    Lungu, Romulus
    Lungu, Mihai
    Efrim, Claudia
    AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 126
  • [32] CONTROL MOMENT GYROS IN ATTITUDE CONTROL
    JACOT, AD
    LISKA, DJ
    JOURNAL OF SPACECRAFT AND ROCKETS, 1966, 3 (09) : 1313 - &
  • [33] Simulation of satellite attitude control using Single Gimbal Control Moment Gyro (SGCMG) system
    Courie, I. A.
    Jenie, Y., I
    Poetro, R. E.
    6TH INTERNATIONAL SEMINAR OF AEROSPACE SCIENCE AND TECHNOLOGY (ISAST), 2018, 1130
  • [34] GEOMETRIC THEORY OF SINGLE-GIMBAL CONTROL MOMENT GYRO SYSTEMS
    MARGULIES, G
    AUBRUN, JN
    JOURNAL OF THE ASTRONAUTICAL SCIENCES, 1978, 26 (02): : 159 - 191
  • [35] Pyramid-Type Single-Gimbal Control Moment Gyro System Singularity Avoidance Using Gimbal Reorientation
    Guo, Jitang
    Geng, Yunhai
    Kong, Xianren
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2020, 43 (06) : 1180 - 1189
  • [36] FEEDBACK-CONTROL AND STEERING LAWS FOR SPACECRAFT USING SINGLE GIMBAL CONTROL MOMENT GYROS
    OH, HS
    VADALI, SR
    JOURNAL OF THE ASTRONAUTICAL SCIENCES, 1991, 39 (02): : 183 - 203
  • [37] FEEDBACK-CONTROL AND STEERING LAWS FOR SPACECRAFT USING SINGLE GIMBAL CONTROL MOMENT GYROS
    OH, HS
    VADALI, SR
    AIAA GUIDANCE, NAVIGATION AND CONTROL CONFERENCE, PTS 1 AND 2: A COLLECTION OF TECHNICAL PAPERS, 1989, : 420 - 430
  • [38] Hybrid Steering Logic for Single-Gimbal Control Moment Gyroscopes
    Leve, Frederick A.
    Fitz-Coy, Norman G.
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2010, 33 (04) : 1202 - 1212
  • [39] Attitude and vibration control with double-gimbal variable-speed control moment gyros
    Sasaki, Takahiro
    Shimomura, Takashi
    Pullen, Sam
    Schaub, Hanspeter
    ACTA ASTRONAUTICA, 2018, 152 : 740 - 751
  • [40] Actuators with Two Double Gimbal Magnetically Suspended Control Moment Gyros for the Attitude Control of the Satellites
    Lungu, Romulus
    Tudosie, Alexandru-Nicolae
    Lungu, Mihai-Aureliu
    Crăciunoiu, Nicoleta-Claudia
    Micromachines, 2024, 15 (09)